US5571343A - Austenitic stainless steel having superior press-formability, hot workability and high temperature oxidation resistance, and manufacturing process therefor - Google Patents
Austenitic stainless steel having superior press-formability, hot workability and high temperature oxidation resistance, and manufacturing process therefor Download PDFInfo
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- US5571343A US5571343A US08/416,875 US41687595A US5571343A US 5571343 A US5571343 A US 5571343A US 41687595 A US41687595 A US 41687595A US 5571343 A US5571343 A US 5571343A
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- 238000004519 manufacturing process Methods 0.000 title claims abstract description 26
- 230000003647 oxidation Effects 0.000 title claims abstract description 24
- 238000007254 oxidation reaction Methods 0.000 title claims abstract description 24
- 229910000963 austenitic stainless steel Inorganic materials 0.000 title claims abstract description 18
- 229910000859 α-Fe Inorganic materials 0.000 claims abstract description 21
- 238000005336 cracking Methods 0.000 claims abstract description 20
- 230000000087 stabilizing effect Effects 0.000 claims abstract description 18
- 238000005098 hot rolling Methods 0.000 claims abstract description 13
- 239000012535 impurity Substances 0.000 claims abstract description 6
- 229910000831 Steel Inorganic materials 0.000 claims description 61
- 239000010959 steel Substances 0.000 claims description 61
- 238000000137 annealing Methods 0.000 claims description 20
- 238000010438 heat treatment Methods 0.000 claims description 9
- 238000000034 method Methods 0.000 claims description 7
- 230000008569 process Effects 0.000 claims description 7
- 239000002253 acid Substances 0.000 claims description 5
- 238000005554 pickling Methods 0.000 claims description 5
- 238000005097 cold rolling Methods 0.000 claims description 3
- 230000007547 defect Effects 0.000 abstract description 15
- 229910001566 austenite Inorganic materials 0.000 abstract description 3
- 230000006872 improvement Effects 0.000 abstract description 2
- 238000012360 testing method Methods 0.000 description 29
- 230000000052 comparative effect Effects 0.000 description 15
- 230000003247 decreasing effect Effects 0.000 description 14
- 239000004615 ingredient Substances 0.000 description 14
- 101100348084 Drosophila melanogaster CDase gene Proteins 0.000 description 12
- 229910052719 titanium Inorganic materials 0.000 description 11
- 239000000203 mixture Substances 0.000 description 10
- 229910001220 stainless steel Inorganic materials 0.000 description 9
- 230000015572 biosynthetic process Effects 0.000 description 7
- 230000007797 corrosion Effects 0.000 description 7
- 238000005260 corrosion Methods 0.000 description 7
- 229910000734 martensite Inorganic materials 0.000 description 6
- 239000002131 composite material Substances 0.000 description 5
- 230000008018 melting Effects 0.000 description 5
- 238000002844 melting Methods 0.000 description 5
- 229910052758 niobium Inorganic materials 0.000 description 5
- 239000010935 stainless steel Substances 0.000 description 5
- 238000005482 strain hardening Methods 0.000 description 5
- 230000000694 effects Effects 0.000 description 4
- 230000006698 induction Effects 0.000 description 4
- 238000002411 thermogravimetry Methods 0.000 description 4
- 229910000589 SAE 304 stainless steel Inorganic materials 0.000 description 3
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 3
- 239000007789 gas Substances 0.000 description 3
- 229910052760 oxygen Inorganic materials 0.000 description 3
- 239000001301 oxygen Substances 0.000 description 3
- 239000000126 substance Substances 0.000 description 3
- 238000005266 casting Methods 0.000 description 2
- 239000010960 cold rolled steel Substances 0.000 description 2
- 229910052750 molybdenum Inorganic materials 0.000 description 2
- 230000009467 reduction Effects 0.000 description 2
- 238000003303 reheating Methods 0.000 description 2
- 229910052715 tantalum Inorganic materials 0.000 description 2
- 238000009864 tensile test Methods 0.000 description 2
- 229910052720 vanadium Inorganic materials 0.000 description 2
- 229910052726 zirconium Inorganic materials 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 239000010953 base metal Substances 0.000 description 1
- 239000000571 coke Substances 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/44—Ferrous alloys, e.g. steel alloys containing chromium with nickel with molybdenum or tungsten
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/42—Ferrous alloys, e.g. steel alloys containing chromium with nickel with copper
Definitions
- the present invention relates to an austenitic stainless steel having superior press-formability, hot workability and high temperature oxidation resistance, and a manufacturing process therefor.
- the austenitic steel which is expressed by 18% Cr-8% Ni (STS 304) is superior in the formability, corrosion resistance and weldability compared with the ferritic stainless steel, and therefore, the austenitic stainless steel is widely used for press-forming purposes.
- the austenitic stainless steel contains a large amount of the expensive element Ni, and therefore, its cost is very high.
- the ingredient ranges are too wide, and therefore, the formability and other properties show much deviations. Further, the contents of C and N are too high, and therefore, the season cracking resistance is unsatisfactory. Particularly, the addition of Cu aggravates the hot workability.
- the present inventor made study and experiments to overcome the disadvantages of the conventional techniques, and came to propose the present invention.
- the object of the present invention to provide an austenitic stainless steel and a manufacturing process therefor, in which, instead of the expensive Ni, there are added Cu as an austenite ( ⁇ ) stabilizing element, tiny amounts of Ti as a ferrite forming element, and B for improvement of high temperature hot workability, so that the optimum Md 30 temperature and the optimum delta-ferrite content can be controlled, thereby improving the formability, the season cracking resistance, the hot workability and the high temperature oxidation resistance, and reducing the surface defects during the hot rolling and saving the manufacturing cost by reducing the content of Ni.
- FIG. 1 is a graphical illustration showing the reduction of the sectional area versus the variation of deformation temperatures
- FIG. 2 illustrates the variation of the weight gain (due to the high temperature oxidation) versus heating time at 1260° C.
- FIG. 3 is a graphical illustration showing the values of the limit drawing ratio (LDR) versus the variation of the austenitic phase stabilizing temperature [Md 30 , (°C.); the temperature at which 50% of a strain-induced martensitic phase ( ⁇ ') are produced under the action of a true strain of 0.3] in a Cu containing steel;
- FIG. 4 is a graphical illustration showing the Erichsen value versus the variation of the stabilizing temperature (Md 30 , °C.) for the austenitic phase in a Cu containing steel;
- FIG. 5 is a graphical illustration showing the variation of the conical cup value (CCV) versus the variation of the stabilizing temperature (Md 30 , °C.) for the austenitic phase in a Cu containing steel;
- FIG. 6 is a graphical illustration showing the variation of the formability versus the variation of the grain size in a cold rolled annealed sheets.
- the austenitic stainless steel according to the present invention includes in weight %: less than 0.07% of C, less than 1.0% of Si, less than 2.0% of Mn, 16-18% of Cr, 6.0-8.0% of Ni, less than 0.005% of Al, less than 0.05% of P, less than 0.005% of S, less than 0.03% of Ti, less than 0.003% of B, less than 3.0% of Cu, less than 0.3% of Mo, less than 0.1% of Nb, less than 0.045% of N, the balance of Fe, and other indispensable impurities.
- the present invention also provides a process for manufacturing the austenitic stainless steel, and the austenitic stainless steel according to the present invention is superior in the press formability, the season cracking resistance, the hot workability and the high temperature oxidation resistance.
- the ingredient C is a stabilizing element for a strong austenitic phase, and, during the casting of a slab or ingot (to be called “slab” below), C lowers the content of the delta-ferritic phase, thereby improving the hot workability. Further, C gives an effect of reducing the contents of expensive Ni, and increases the stacking fault energy, thereby improving the formability. If its content is too high, the strain-induced martensite strength is increased during the deep-drawing process, and the residue stress becomes high, with the result that the season cracking resistance is decreased. Further, during the annealing, the decrease of the corrosion resistance due to the carbide precipitation is apprehended. Therefore, the content of C should be desirably limited to less than 0.07%.
- the ingredient Si is advantageous for the high temperature oxidation resistance, but, if its content is too high, the content of the delta-ferrite is increased, with the result that the hot workability is decreased. Further, the Si inclusions are increased, so that the formation of the inclusion-induced sliver would be apprehended. Therefore, the content of Si should be preferably limited to less than 1.0%.
- the content of Mn should be preferably less than 2.0%.
- the content of the ingredient Cr should be preferably limited to 16.0-18.0%.
- the content of Ni is adjusted by taking into account the stability of the austenitic phase, the formability, the season cracking resistance and the manufacturing cost. If its content is too high, the Md 30 temperature becomes too low, so that the stretchability would be decreased, as well as increasing the manufacturing cost. If its content is too low, the formation of the strain-induced martensitic phase is increased, with the result that the season cracking resistance is decreased. Therefore, the content of Ni should be preferably limited to 6.0-8.0%.
- the ingredient Al is for improving the high temperature oxidation resistance.
- the ingredient Cu softens the steel, increases the stacking fault energy, and raises the stability of the austenitic phase. Therefore, Cu can be used in place of Ni, and if its content is more than 3.0%, then the formability is decreased, and the low melting point Cu is segregated on the boundary of the grains during the casting of the slab, so that cracks would be apprehended during the hot rolling. Therefore, its content should be preferably limited to less than 3.0%.
- the content of P is too high, the formability and the corrosion resistance are aggravated, and therefore, its content should be preferably limited to less than 0.05%.
- the ingredient S lowers the hot rollability, and particularly, is segregated on the grain boundary of the austenitic phase during the solidification, so that slivers would be formed during the hot rolling. Therefore its content should be preferably limited to less than 0.005%.
- the ingredient Ti serves the role of preventing the surface defects during the hot rolling by preventing the high temperature corrosion during the heating of the slab. Further it inhibits the formation of an orange peel by making the grains fine. Further if a steel contains a tiny amount of Ti which stabilizes the ferrite at the same stabilizing temperature Md 30 , the formation of a strain-induced martensitic phase is increased during the press-forming compared with a steel without containing Ti. Consequently, the rupture strength and the work hardening exponent n of the high strain region are increased, so that the formability would be improved. If the content of Ti is too high, surface defects due to Ti oxides are caused, and therefore, the content of Ti should be preferably limited to 0.03%.
- the ingredient B gives the effect of improving the hot workability, and therefore it is effective in preventing the surface defects caused during the hot workability. However, if its content is too high, it produces B compounds, so that the melting point of the steel would be significantly decreased, thereby aggravating the hot workability. Therefore, the content of B should be preferably limited to less than 0.003%.
- the content of N is high, it helps reduce the delta-ferrite, but it gives the effect of raising the yield strength of the steel by twice the effect of C, so that the formability would be aggravated. Further, due to the rise in the hardness and strengths, the season cracking resistance is decreased, and therefore, the content of N should be preferably limited to less than 0.045%.
- the ingredients Mo and Nb are contained for an unavoidable reason, and therefore, it will be better, the less they are contained.
- the contents of Mo and Nb should be preferably limited to 0.3% and 0.1% respectively.
- Md 30 (°C.) which represents the stability of the austenitic phase is high, the strain-induced martensitic phase is produced very much during the press-forming. Therefore, if the formability is to be improved, the Md 30 temperature should be controlled to the optimum level.
- the formability is decreased. Then the content of the expensive Ni should be raised, and therefore, the manufacturing cost is increased. If the Md 30 temperature is too high, the formability is not only aggravated, but also the season cracking resistance is aggravated, with the result that the season cracks are formed after the press-forming.
- the Md 30 temperature should be preferably limited to -10° to +15 (°C.).
- the hot workability is decreased, with the result that surface defects are generated during the manufacturing of the hot rolled steel sheet. Further, in manufacturing a cold rolled steel sheet, if the content of the delta-ferrite becomes high, the yield strength is increased, so that the formability would be decreased. Therefore the adjustment of the content of the delta-ferrite to the optimum level is important.
- the content of the delta-ferrite should be preferably limited to less than 9.0 vol %.
- the content (vol %) of the delta-ferrite within the slab is expressed by: [ ⁇ (Cr %+Mo %+1.5 Si %+0.5 Nb %+18)/(Ni %+0.52 Cu %+30 C %+30 N %+0.5 Mn %+360 ⁇ +0.262] ⁇ 161-161.
- the austenitic stainless steel of the present invention is manufactured with the same process as that of the STS 304 steel, i.e., through a hot rolling of a slab, an annealing of the hot rolled steel sheet, an acid pickling, a cold rolling, an annealing of the cold rolled steel sheet, an acid pickling, and a skin pass.
- the preferred manufacturing conditions are as follows.
- the reheating temperature for the steel slab should be preferably over 1250° C., and more preferably 1250°-1270° C.
- the Cr content which promotes the high temperature oxidation resistance is lower by 1% compared with the STS 304 steel. Therefore, if the reheating temperature is as high as that for the STS 304 steel (1270°-1290°C.), then the probability of producing the surface defects due to the increase of the high temperature oxidation is very high, and therefore, a low temperature heating (1250°-1270°C.) is required.
- the hot rolling deformation resistance is low at the high temperature owing to the 2% addition of Cu, and therefore, there occur no rough band defects which are caused by an excessive deformation resistance during a hot rolling and by the load of the roll or by the roll fatigue.
- the annealing temperature for the hot rolled sheet should be preferably 1100°-1180° C.
- the annealing temperature for the cold rolled sheet should be preferably 1000°-1150° C.
- the annealing conditions for the cold rolled sheet are closely related to the grain size of the final product.
- the annealing conditions for the cold rolled sheet is controlled in the following manner. That is, the grain size should be preferably same as that of ASTM No. 6.5-10.0, and more preferably ASTM No. 8.0-9.0.
- Austenitic stainless steels having the compositions of Table 1 were melted in a vacuum induction melting furnace having a capacity of 50 kg, and then ingots of 25 kg were formed.
- the conventional steels C and D they were heated at 1290° C. for 2 hours, and were hot-rolled, thereby manufacturing hot rolled sheets of 2.5 mm.
- the inventive steels 1 and 2 and the comparative steels A and B they were heated at 1270° C. for 2 hours, and were hot-rolled, thereby manufacturing hot rolled sheets of 2.5 mm. Then all of them were annealed at a temperature of 1100° C., and then, the hot rolled sheets were acid-pickled.
- the ingots of the inventive steel 1 and the comparative steel A were heated at 1270° C. for 2 hours, and the ingot of the conventional steel C was heated at 1290° C. for 2 hours. Then they were hot-rolled into 15 mm sheets, and then, they were processed into gleeble test pieces having a diameter of 10 mm. Then they were evaluated as to the hot workability by using a gleeble testing instrument, and the test results are shown in Table 1 below.
- the temperature was raised at 10° C./sec up to the high temperature testing level, and then, the temperature was maintained for 10 seconds. Then a high temperature tensile strength test was carried out at 30 mm/sec deformation speed. Then the sectional area of the broken test piece was measured so as to calculate the sectional area reduction rate.
- the inventive steels 1 and 2 in which Ti and B were added were superior in the limit drawing ratio (LDR), the stretchability (Erichsen) and the composite formability (CCV) compared with the comparative steels A and B and the conventional steels C and D in which Ti and B were not added.
- LDR limit drawing ratio
- Erichsen stretchability
- CCV composite formability
- the steels of the present invention showed more than the same level as those of the comparative steels A and B and the conventional steels C and D.
- the reason why a tiny amounts of Ti and B improves the formability is that, if Ti which is a ferrite stabilizing element is added, the formation of the strain-induced martensite is increased compared with a non-added steel at the same Md 30 , with the result that the rupture strength and the work hardening exponent n are increased, thereby improving the formability.
- inventive steels 1 and 2 showed a high tensile strength and a low yield ratio (yield strength/tensile strength). Particularly, at the 40-30% elongation region which is the high deformation region, the value of the work hardening exponent n was high, and therefore, ruptures did not occur during the press-forming, with the result that the formability was improved.
- inventive steels 1 and 2 and the comparative steels A and B which contained Cu were low in the yield strength compared with the conventional steels C and D. Further, they could be easily press-formed in the initial stage of the press-forming because the work hardening exponent n was low in the low deformation region of 20-10% elongation range, while in the later stage, the local necking could be prevented so as to improve the formability, because the work hardening exponent n becomes high in the high deformation region of 40-30% elongation range.
- the inventive steel 1 is far excellent in the hot workability compared with the comparative steel A, and is same in the hot workability as that of the conventional steel D.
- the reason why the addition of Ti and B improves the hot workability as in the case of the inventive steel 1 is as follows. That is, if Cu which is a low melting point element is added, the grain boundary bonding strength is lowered during a high temperature heating as in the case of heating the ingot to a temperature of 1290° C. However, if a tiny amount of Ti is added, the grains at the high temperature is made fine, as well as preventing the grain boundary oxidation. Further, Ti is bonded with N in the melt, so that the content of N which lowers the hot workability would be reduced. When B is added together with Ti, B is segregated on the grain boundary so as to inhibit the cavitation of the grain boundary and so as to delay the decohesion of the grain boundary. Further, in a solid solution state, the interaction between B and the vacancy improves the hot workability.
- Austenitic stainless steels having the compositions of Table 3 below were melted in a vacuum induction melting furnace having a capacity of 50 kg so as to manufacture ingots of 25 kg. Then the ingots were heated at a temperature of 1270° C. for 2 hours, and then, a hot rolling was carried out to manufacture hot rolled sheets of 2.5 mm. Then they were annealed at a temperature of 1100° C., and then, an acid-wash was carried out. Then test pieces for a thermo-gravimetric analysis (TGA) were prepared to carry out the TGA, and the results are shown in FIG. 2.
- TGA thermo-gravimetric analysis
- the testing atmosphere was a mixture of gases (cokes oven gas plus blast furnace gas) (C.O.G.+B. F. G.), and the excess oxygen volume ratio was 3%, while the oxidation testing temperature was 1260° C.
- the inventive steel 3 was superior in the high temperature oxidation resistance compared with the comparative steel E.
- the reason is not that Ti is concentrated within the scales to enhance the oxidation resistance, but that the oxygen existing on the grain boundary is prevented from being moved into the base metal.
- Austenitic stainless steels having the compositions of Table 4 below were melted in a vacuum induction furnace having a capacity of 30 kg so as to manufacture ingots. Then they were heated at 1260° C. for 2 hours, and then, they were hot-rolled into 2.5 mm. Then an annealing was carried out at 1110° C. so as to prepare hot rolled annealed sheets. Then they were acid-pickled, and then, were cold-rolled into a thickness of 0.5 mm. Then an annealing was carried out at a temperature of 1110° C., thereby manufacturing cold rolled annealed steel sheets. Then they were acid-pickled, and then, a skin pass was carried out. Then they were subjected to a formability test, and the results are shown in FIGS. 3 to 5.
- FIG. 3 illustrates the variation of the limit drawing ratio (LDR) versus the variation of the stabilizing temperature [Md 30 (°C.)] for the austenitic phase.
- FIG. 4 illustrates the variation of the Erichsen value, and
- FIG. 5 illustrates the variation of the conical cup value (CCV).
- the Erichsen value which shows the stretch ability increases.
- the Erichsen value shows the maximum level, and thereafter, the Erichsen value gradually drops.
- the conical cup value (CCV) which indicates the composite formability shows the minimum level at the point where the temperature Md 30 is 0° C., and thus, shows that the composite formability is most superior at the point. Thereafter, the conical cup value increases, thereby showing that the composite formability is aggravated.
- Austenitic steels having the compositions of Table 5 were melted in a vacuum induction furnace having a capacity of 30 kg so as to manufacture ingots.
- a heating was carried out at a temperature of 1260° C. for 2 hours, while in the case of the comparative steel I, a heating was carried out at a temperature of 1290° C. for 2 hours.
- a hot rolling was carried out into 2.5 mm, and then, an annealing was carried out at 1110° C.
- an acid pickling was carried out, and then, a cold rolling was carried out into 0.7 mm cold rolled sheets.
- annealings were carried out with variation of the annealing time. Then the LDR and Erichsen value versus the variation of the grain sizes were tested, and the results are shown in FIG. 6.
- the inventive steel 7 showed a superior formability compared with the conventional steel I, and the formability was most superior in the grain size range of ASTM 8-9.
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Abstract
Description
TABLE 1
__________________________________________________________________________
Composition (wt %)
Test piece
C Si Mn P S Cr Ni Mo Ti Cu
__________________________________________________________________________
Inventive
1 0.041
0.66
1.32
0.02
0.002
17.25
7.42
0.13
0.017
1.91
2 0.062
0.62
1.31
0.02
0.002
17.29
7.33
0.13
0.017
1.92
Comparative
A 0.042
0.61
1.28
0.02
0.001
17.43
7.32
0.13
-- 1.90
B 0.066
0.63
1.27
0.02
0.002
17.56
7.35
0.13
-- 1.90
Conventional
C 0.045
0.61
1.16
0.02
0.002
18.39
8.73
0.10
-- 0.20
D 0.050
0.56
1.34
0.02
0.002
18.26
8.26
0.16
-- 0.21
__________________________________________________________________________
Delta-**
Composition (wt %)
Md.sub.30 *
ferrite
Test piece
Al B N (°C.)
(vol %)
Remarks
__________________________________________________________________________
Inventive
1 0.001
0.0028
0.0166
-2.1 6.41 Ti, B
2 0.001
0.0023
0.0228
-12.6
4.12 Added steel
Comparative
A 0.001
-- 0.0168
-0.4 7.00 Ti, B
B 0.001
-- 0.0138
-12.2
5.80 Non-added steel
Conventional
C 0.001
-- 0.0386
-15.4
6.86 STS304
D 0.001
-- 0.0403
-4.4 6.83
__________________________________________________________________________
*Md.sub.30 (°C.) = 551-462(C % + N %)--9.2 Si %--8.1 Mn %--29(Ni %
+ Cu %)--13.8 Cr %--18.5 Mo %--68 Nb %--1.42(ASTM No. 8.0).
**Deltaferrite(vol %) within the slab = [((Cr % + Mo % + 1.5 Si % + 0.5 N
% + 18)/(Ni % + 0.52 Cu % + 30 C % + 30 N % + 0.5 Mn % + 36)) + 0.262]
× 161--161.
TABLE 2
__________________________________________________________________________
Formability Tensile test
Thick- Yield Tensile
Md.sub.30
ness Erichsen,
CCV,
Seasn
str str
Test piece
(°C.)
(mm)
LDR
mm mm crckng
(kg/mm.sup.2)
(kg/mm.sup.2)
__________________________________________________________________________
Inventive
1 -2.1
0.7 2.02
12.8 26.3
3.30
26.20 63.07
2 -12.6
0.7 1.98
13.1 26.5
2.78
26.97 63.27
Comparative
A -0.4
0.7 1.98
12.7 26.7
3.03
26.85 61.13
B -12.2
0.7 1.94
13.0 26.7
2.78
26.67 60.67
Conventional
C -15.4
0.7 1.90
11.8 27.3
2.78
27.10 64.40
D -4.4
0.7 1.90
12.0 27.3
-- 30.13 67.10
__________________________________________________________________________
Tensile test
Yield Harding exp.
Hard-
ratio Elongtn
20-10%
40-30%
ness
Test piece
(Y.S/T.S)
(%) elongtn
elongtn
(Hv) Remarks
__________________________________________________________________________
Inventive
1 0.415 54.50 0.38 0.59 145 Ti, B
2 0.426 55.77 0.41 0.52 154 Added steel
Comparative
A 0.439 55.57 0.38 0.56 148 Ti, B
B 0.440 56.37 0.39 0.51 153 Non-added Steel
Conventional
C 0.421 54.27 0.42 0.50 170 STS304
D 0.449 52.67 0.39 0.50 175
__________________________________________________________________________
1. The limit drawing ratio(LDR) test: a punch diameter <50 mm>, lubricant
<Fatty oil>.
2. Erichsen test: based on JIS Z 2247
3. Conical cup test (CCV): based on JIS Z 2249.
4. Season cracking test: Blank diameter variation: <80, 87.5, 95 mm>,
punch diameter: <50, 38, 28.8 mm>, season cracking test: <after a
multistep pressforming, the test piece was left in the outer atmosphere,
and the limit drawing ratio at which cracks are formed was indicated.
5. Tensile strength test: the test piece size was based on JIS 13B, and
the tensile speed was 20 mm/min.
TABLE 3
__________________________________________________________________________
Chemical composition (wt %) Md.sub.30 *
Test piece
C Si Mn P S Cr Ni Mo Ti Cu Al B N (°C.)
__________________________________________________________________________
Inventive
3 0.060
0.64
1.33
0.02
0.02
17.15
7.37
0.13
0.019
1.95
0.002
0.0014
0.0195
-10.9
Comparative
E 0.052
0.62
1.31
0.02
0.01
17.15
7.37
0.13
-- 1.92
0.001
-- 0.0135
-1.9
__________________________________________________________________________
*Md.sub.30 is same that which is presented in Table 1 of Example 1.
TABLE 4
__________________________________________________________________________
Chemical composition (wt %) Md.sub.30 *
Test piece
C Si Mn P S Cr Ni Mo Ti Cu Al B N (°C.)
__________________________________________________________________________
Comparative
F 0.054
0.55
1.25
0.02
0.02
16.84
6.79
0.20
0.017
1.90
0.001
0.0023
0.0167
18.72
G 0.060
0.51
1.54
0.02
0.02
17.16
6.61
0.20
0.017
1.91
0.001
0.0022
0.0191
15.27
Inventive
4 0.055
0.62
1.23
0.02
0.02
16.58
7.10
0.19
0.017
1.90
0.001
0.0024
0.0190
11.05
5 0.068
0.54
1.28
0.02
0.01
16.97
6.47
0.20
0.017
1.96
0.001
0.0022
0.0417
5.75
6 0.057
0.58
1.24
0.02
0.02
16.58
7.59
0.20
0.017
1.90
0.001
0.0023
0.0125
-0.7
Comparative
H 0.063
0.52
1.26
0.02
0.01
16.93
8.10
0.20
0.017
1.91
0.001
0.0022
0.0197
-26.4
__________________________________________________________________________
*Md.sub.30 (°C.) = 551-462(C % + N %)--9.2 Si %--8.1 Mn %--29(Ni %
+ Cu %)--13.8 Cr %--18.5 Mo %--68 Nb %--1.42(ASTM grain No. 8.0).
TABLE 5
__________________________________________________________________________
Chemical composition (wt %)
Test piece
C Si Mn P S Cr Ni Mo Ti Cu Al B N Md.sub.30
__________________________________________________________________________
°C.
Inventive
7 0.042
0.65
1.31
0.021
0.001
16.68
7.65
0.05
0.014
2.01
0.002
0.0020
0.0134
-1.48
Conventional
I 0.049
0.53
1.04
0.026
0.003
18.15
8.57
0.10
0.014
0.20
0.001
0.0027
0.0427
-8.05
__________________________________________________________________________
Claims (9)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| KR1019930016607A KR950009223B1 (en) | 1993-08-25 | 1993-08-25 | Austenitic stainless steel with excellent press formability, hot workability and high temperature oxidation resistance |
| KR1993/16607 | 1993-08-25 | ||
| PCT/KR1994/000114 WO1995006142A1 (en) | 1993-08-25 | 1994-08-24 | Austenitic stainless steel having superior press-formability, hot workability and high temperature oxidation resistance, and manufacturing process therefor |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US5571343A true US5571343A (en) | 1996-11-05 |
Family
ID=19361958
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US08/416,875 Expired - Fee Related US5571343A (en) | 1993-08-25 | 1995-04-19 | Austenitic stainless steel having superior press-formability, hot workability and high temperature oxidation resistance, and manufacturing process therefor |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US5571343A (en) |
| JP (1) | JP2693274B2 (en) |
| KR (1) | KR950009223B1 (en) |
| CN (1) | CN1040669C (en) |
| TW (1) | TW314556B (en) |
| WO (1) | WO1995006142A1 (en) |
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| US6274084B1 (en) * | 1998-07-02 | 2001-08-14 | Ugine Sa | Corrosion-resistant low-nickel austenitic stainless steel |
| EP1156125A3 (en) * | 2000-05-16 | 2002-01-30 | Nisshin Steel Co., Ltd. | Austenitic stainless steel excellent in fine blankability |
| US6358338B1 (en) * | 1999-07-07 | 2002-03-19 | Usinor | Process for manufacturing strip made of an iron-carbon-manganese alloy, and strip thus produced |
| EP1249513A1 (en) * | 2001-04-12 | 2002-10-16 | Nisshin Steel Co., Ltd. | A soft stainless steel sheet excellent in workability |
| US20030021716A1 (en) * | 2001-07-27 | 2003-01-30 | Usinor | Austenitic stainless steel for cold working suitable for later machining |
| US6562153B1 (en) * | 1999-10-04 | 2003-05-13 | Hitachi Metals, Ltd. | Strain-induced type martensitic steel having high hardness and having high fatigue strength |
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Cited By (36)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6222286B1 (en) * | 1994-08-01 | 2001-04-24 | Nisshin Steel Co., Ltd. | Stepping motor with rust inhibiting and eddy current minimizing characteristics |
| US5709759A (en) * | 1995-04-21 | 1998-01-20 | Avesta Sheffield Aktiebdag (Publ) | Method of working a hot-rolled strip |
| US6274084B1 (en) * | 1998-07-02 | 2001-08-14 | Ugine Sa | Corrosion-resistant low-nickel austenitic stainless steel |
| US6358338B1 (en) * | 1999-07-07 | 2002-03-19 | Usinor | Process for manufacturing strip made of an iron-carbon-manganese alloy, and strip thus produced |
| US6562153B1 (en) * | 1999-10-04 | 2003-05-13 | Hitachi Metals, Ltd. | Strain-induced type martensitic steel having high hardness and having high fatigue strength |
| KR100421511B1 (en) * | 2000-05-16 | 2004-03-09 | 닛신 세이코 가부시키가이샤 | Austenitic stainless steel excellent in fine blankability |
| EP1156125A3 (en) * | 2000-05-16 | 2002-01-30 | Nisshin Steel Co., Ltd. | Austenitic stainless steel excellent in fine blankability |
| SG108254A1 (en) * | 2000-05-16 | 2005-01-28 | Nisshin Steel Co Ltd | Austenitic stainless steel excellent in fine blankability |
| US20170164426A1 (en) * | 2000-08-17 | 2017-06-08 | Ati Properties Llc | Austenitic stainless steels including molybdenum |
| SG96687A1 (en) * | 2001-04-12 | 2003-06-16 | Nisshin Steel Co Ltd | A soft stainless steel sheet excellent in workability |
| EP1249513A1 (en) * | 2001-04-12 | 2002-10-16 | Nisshin Steel Co., Ltd. | A soft stainless steel sheet excellent in workability |
| KR100473072B1 (en) * | 2001-04-12 | 2005-03-08 | 닛신 세이코 가부시키가이샤 | A soft stainless steel sheet excellent in workability |
| US20040213665A1 (en) * | 2001-05-10 | 2004-10-28 | Shinjiro Ohishi | Exhaust gas assembly with improved heat resistance for vgs turbocharger, method for manufacturing heat resisting member applicable thereto, and method for manufacturing shaped material for adjustable blade applicable thereto |
| US20090145523A1 (en) * | 2001-05-10 | 2009-06-11 | Shinjiro Ohishi | Method for manufacturing heat resisting member applicable to an exhaust gas guide assembly with improved heat resistance for VGS turbocharger |
| US20030021716A1 (en) * | 2001-07-27 | 2003-01-30 | Usinor | Austenitic stainless steel for cold working suitable for later machining |
| FR2827876A1 (en) * | 2001-07-27 | 2003-01-31 | Usinor | AUSTENITIC STAINLESS STEEL FOR COLD DEFORMATION THAT CAN BE FOLLOWED BY MACHINING |
| EP1281785A3 (en) * | 2001-07-27 | 2003-05-14 | Usinor | Austenitic stainless steel for cold deformation which may be followed by machining |
| US20100119403A1 (en) * | 2001-07-27 | 2010-05-13 | Ugitech | Austenitic Stainless Steel for Cold Working Suitable For Later Machining |
| US20120237388A1 (en) * | 2009-11-18 | 2012-09-20 | Sumitomo Metal Industries, Ltd. | Austenitic stainless steel sheet and a method for its manufacture |
| CN101949474B (en) * | 2010-02-05 | 2012-05-09 | 西峡县西泵特种铸造有限公司 | Heat-resistant stainless steel exhaust pipe and preparation method thereof |
| US8845824B2 (en) | 2011-07-25 | 2014-09-30 | Hyundai Motor Company | Austenitic heat-resisting cast steel and exhaust manifold using the same |
| CN103100562B (en) * | 2011-11-09 | 2015-04-01 | 宁波宝新不锈钢有限公司 | Method of machining special passivated stainless steel surface |
| CN103100562A (en) * | 2011-11-09 | 2013-05-15 | 宁波宝新不锈钢有限公司 | Method of machining special passivated stainless steel surface |
| US10378078B2 (en) | 2015-12-28 | 2019-08-13 | The Nanosteel Company, Inc. | Delayed cracking prevention during drawing of high strength steel |
| CN105414186A (en) * | 2015-12-28 | 2016-03-23 | 东台市江龙金属制造有限公司 | High-hardness steel plate machining method |
| CN105598640A (en) * | 2015-12-28 | 2016-05-25 | 东台市江龙金属制造有限公司 | Method for processing high-hardness gasket |
| WO2017117128A1 (en) * | 2015-12-28 | 2017-07-06 | The Nanosteel Company, Inc. | Delayed cracking prevention during drawing of high strength steel |
| US11254996B2 (en) | 2015-12-28 | 2022-02-22 | United States Steel Corporation | Delayed cracking prevention during drawing of high strength steel |
| US20180106557A1 (en) * | 2016-03-28 | 2018-04-19 | Lg Electronics Inc. | Stainless steel and pipe made thereof |
| CN108200771A (en) * | 2016-03-28 | 2018-06-22 | Lg电子株式会社 | Stainless steel and the piping being made of the stainless steel |
| US10627168B2 (en) * | 2016-03-28 | 2020-04-21 | Lg Electronics Inc. | Stainless steel and pipe made thereof |
| CN107419261B (en) * | 2017-07-04 | 2020-08-18 | 当涂县宏宇金属炉料有限责任公司 | Processing method for stably improving surface anti-pollution capability of stainless steel product |
| CN107419261A (en) * | 2017-07-04 | 2017-12-01 | 当涂县宏宇金属炉料有限责任公司 | A kind of stable processing method for improving stainless steel product surface anti-pollution ability |
| CN111893267A (en) * | 2020-07-28 | 2020-11-06 | 西安建筑科技大学 | A method for formulating heating parameters that explicitly considers organizational goals and requirements |
| CN111893267B (en) * | 2020-07-28 | 2022-04-26 | 西安建筑科技大学 | A method for formulating heating parameters that explicitly considers organizational goals and requirements |
| WO2023210959A1 (en) * | 2022-04-29 | 2023-11-02 | 주식회사 포스코 | Austenitic stainless steel |
Also Published As
| Publication number | Publication date |
|---|---|
| CN1040669C (en) | 1998-11-11 |
| KR950006015A (en) | 1995-03-20 |
| TW314556B (en) | 1997-09-01 |
| CN1113661A (en) | 1995-12-20 |
| KR950009223B1 (en) | 1995-08-18 |
| JP2693274B2 (en) | 1997-12-24 |
| JPH08501352A (en) | 1996-02-13 |
| WO1995006142A1 (en) | 1995-03-02 |
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